Passive Damping of Solar Array Vibrations Using Hyperelastic Shape Memory Alloy with Multilayered Viscous Lamina

IF 0.1 4区 工程技术 Q4 ENGINEERING, AEROSPACE Aerospace America Pub Date : 2023-08-10 DOI:10.3390/aerospace10080704
Jae-Hyeon Park, Sung-Woo Park, Jong-Pil Kim, Hyun-Ung Oh
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Abstract

A novel passive vibration-damping device is proposed and investigated for a large deployable solar array. One strategy for achieving high damping in a solar panel is using a yoke structure comprising a hyperelastic shape memory alloy and multiple viscous adhesive layers of acrylic tape. The effectiveness of the proposed system in achieving a high damping performance was demonstrated by conducting free vibration and low-level sine sweep tests using a solar array, and a 0.75-m-long flexible dummy structure was simulated. We also investigated the dependence of the damping performance of the proposed structure on the number of viscous lamina layers. Finally, the damping characteristics of the proposed system were assessed under predictable on-orbit temperature conditions.
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多层粘层超弹性形状记忆合金对太阳能电池阵振动的被动阻尼
提出并研究了一种用于大型可展开太阳能电池阵的新型被动减振装置。在太阳能电池板中实现高阻尼的一种策略是使用包含超弹性形状记忆合金和丙烯酸胶带的多个粘性粘合层的轭形结构。利用太阳能电池阵列进行自由振动和低阶正弦扫描试验,验证了该系统在实现高阻尼性能方面的有效性,并对一个0.75 m长的柔性假体结构进行了仿真。我们还研究了所提出的结构的阻尼性能与粘性层数的关系。最后,在可预测的在轨温度条件下,对系统的阻尼特性进行了评估。
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来源期刊
Aerospace America
Aerospace America 工程技术-工程:宇航
自引率
0.00%
发文量
9
审稿时长
4-8 weeks
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